[go: up one dir, main page]

JP2013029077A - Method of manufacturing hollow structural member and combustor having hollow structural member - Google Patents

Method of manufacturing hollow structural member and combustor having hollow structural member Download PDF

Info

Publication number
JP2013029077A
JP2013029077A JP2011165698A JP2011165698A JP2013029077A JP 2013029077 A JP2013029077 A JP 2013029077A JP 2011165698 A JP2011165698 A JP 2011165698A JP 2011165698 A JP2011165698 A JP 2011165698A JP 2013029077 A JP2013029077 A JP 2013029077A
Authority
JP
Japan
Prior art keywords
structural member
metal
manufacturing
hollow structural
substrate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2011165698A
Other languages
Japanese (ja)
Other versions
JP5931368B2 (en
Inventor
Masaki Taneike
正樹 種池
Ikuo Okada
郁生 岡田
Hidetaka Oguma
英隆 小熊
Tsuguo Hasegawa
貢生 長谷川
Toshio Fujii
敏生 藤井
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2011165698A priority Critical patent/JP5931368B2/en
Publication of JP2013029077A publication Critical patent/JP2013029077A/en
Application granted granted Critical
Publication of JP5931368B2 publication Critical patent/JP5931368B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Coating By Spraying Or Casting (AREA)

Abstract

PROBLEM TO BE SOLVED: To provide a method of manufacturing a hollow structural member and a combustor having the hollow structural member, capable of shortening a manufacturing time, and capable of improving workability.SOLUTION: This method of manufacturing an inner cylinder having a cooling hole 4 includes a bent plate installation preparing process S1 and a bent plate installation process S2 of installing a bent plate 10 bent to extend along the surface of a thin plate 22 and project from the surface, on the surface of the thin plate, a metal flame-spraying process S3 of manufacturing the hollow structural member 20 by forming a plane 23 on the surface of the thin plate 22 by flame-spraying molten metal M to the bent plate 10 arranged on the surface of the thin plate 22, and a cylinder shape forming process S4 of forming the hollow structural member 20 in a cylindrical shape.

Description

本発明は、耐熱の中空構造部材の製造方法、及びこの中空構造部材を備えた燃焼器に関するものである。   The present invention relates to a method for manufacturing a heat-resistant hollow structural member, and a combustor including the hollow structural member.

例えば、ガスタービンの燃焼器においては、燃焼室を構成する内筒、外筒、及び尾筒などの筒状部材は常時高温に曝されるため、高い耐熱性が要求される。このため、これら筒状部材は中空構造とされ、この中空構造部分に空気や蒸気等の冷却媒体を流通させることによって、筒状部材の冷却を行なっている。   For example, in a combustor of a gas turbine, since cylindrical members such as an inner cylinder, an outer cylinder, and a tail cylinder constituting a combustion chamber are constantly exposed to high temperatures, high heat resistance is required. For this reason, these cylindrical members are made into a hollow structure, and cooling a cylindrical member is carried out by distribute | circulating cooling media, such as air and a vapor | steam, to this hollow structure part.

ここで、従来より、このような中空構造を有する筒状部材は、中空構造を有する板状部材、即ち中空構造板をプレス加工して所定の大きさの筒状に形成した後に、中空構造板の端縁同士を突き合わせて溶接することによって製造されている。また、この中空構造板の製造方法は、例えば特許文献1に開示されており、具体的には、一枚又は二枚の金属板表面に凹溝を放電加工等によって形成し、二枚の金属板の間に凹溝が配置するようにこれら二枚の金属板を張り合わせてロウ付けによって接合するものである。   Here, conventionally, the cylindrical member having such a hollow structure is a plate-shaped member having a hollow structure, that is, after the hollow structure plate is formed into a cylindrical shape of a predetermined size by pressing. Are manufactured by butting the edges of each other. Moreover, this hollow structure plate manufacturing method is disclosed in, for example, Patent Document 1, and specifically, a groove is formed on one or two metal plate surfaces by electric discharge machining or the like, and two metal plates are formed. These two metal plates are laminated and joined by brazing so that a concave groove is disposed between the plates.

特開2008−200836号公報Japanese Patent Laid-Open No. 2008-200836

しかしながら、上記特許文献1の中空構造板の製造方法においては、金属板への凹溝加工、及び、ロウ付けといった工程を経て板状部材が製造されるため、工程が複雑であり、製造に時間を要していた。さらに、ロウ付け材料を使用することによって中空構造板の延性が低下するため、プレス加工による加工性が好ましくないという問題があった。   However, in the manufacturing method of the hollow structure plate of Patent Document 1, since the plate-like member is manufactured through processes such as the groove processing on the metal plate and brazing, the process is complicated and time is required for manufacturing. Needed. Furthermore, since the ductility of the hollow structure plate is reduced by using a brazing material, there is a problem that workability by press working is not preferable.

本発明はこのような事情を考慮してなされたもので、製造時間短縮と加工性の向上とを達成できる中空構造部材の製造方法、及びこの中空構造部材を備えた燃焼器を提供することを目的とする。   The present invention has been made in view of such circumstances, and provides a method for manufacturing a hollow structure member that can achieve a reduction in manufacturing time and an improvement in workability, and a combustor including the hollow structure member. Objective.

上記課題を解決するため、本発明は以下の手段を採用している。
即ち、本発明に係る中空構造部材の製造方法は、中空孔を有する板材である中空構造部材の製造方法であって、第一基板の表面上に、該表面に沿って延在するとともに該表面から突出するように屈曲する屈曲板を設置する設置工程と、前記表面及び該表面上に配置された前記屈曲板に対して溶融金属を溶射することによって、前記第一基板に第二基板を積層する溶射工程とを備えることを特徴とする。
In order to solve the above problems, the present invention employs the following means.
That is, the method for producing a hollow structural member according to the present invention is a method for producing a hollow structural member that is a plate having a hollow hole, and extends along the surface of the first substrate and extends to the surface. An installation step of installing a bending plate that is bent so as to protrude from the surface, and laminating a second substrate on the first substrate by spraying molten metal on the surface and the bending plate disposed on the surface And a thermal spraying process.

このような中空構造部材の製造方法によれば、第一基板の表面上に屈曲板を設置し、その後に金属溶射により第二基板を積層することで、容易に中空構造部材を製造することができる。従って、少ない製造工程によって確実に中空構造部材を製造することができる。また、上記設置工程及び溶射工程においては、ロウ付け材料等の接合材を用いないため、中空構造部材の延性低下等の材料特性に影響を与えることがなく、プレス加工を容易に行うことができる。   According to such a method for manufacturing a hollow structural member, it is possible to easily manufacture the hollow structural member by installing a bent plate on the surface of the first substrate and then laminating the second substrate by metal spraying. it can. Therefore, it is possible to reliably manufacture the hollow structure member with a small number of manufacturing steps. Further, in the installation step and the thermal spraying step, since a bonding material such as a brazing material is not used, it is possible to easily perform the press work without affecting the material properties such as the ductility deterioration of the hollow structure member. .

また、前記屈曲板が、セラミック材料よりなり、前記屈曲板を溶解して除去する溶解工程をさらに備えていてもよい。   The bending plate may be made of a ceramic material, and may further include a melting step of dissolving and removing the bending plate.

セラミック材料よりなる屈曲板を設置することによって、設置工程の手間を省略でき、さらなる製造工程短縮につながる。   By installing a bent plate made of a ceramic material, the labor of the installation process can be omitted, leading to further shortening of the manufacturing process.

さらに、前記第一基板が円筒形状をなし、前記設置工程は前記第一基板の外周面に前記屈曲板を設置する工程であり、前記溶射工程は前記第一基板の外周面に前記第二基板を積層する工程であってもよい。   Further, the first substrate has a cylindrical shape, the installation step is a step of installing the bent plate on the outer peripheral surface of the first substrate, and the spraying step is performed on the outer peripheral surface of the first substrate. May be a step of laminating.

第一基板が円筒形状であることによって、中空構造を有する筒状部材を、製造工程を短縮しながら製造することができる。   When the first substrate has a cylindrical shape, a cylindrical member having a hollow structure can be manufactured while shortening the manufacturing process.

また、前記第二基板が、前記第一基板側に配置される第一の金属よりなる第一金属層と、前記第一金属層に積層され、前記第一の金属とは異なる第二の金属よりなる第二金属層とを有していてもよい。   The second substrate is a first metal layer made of a first metal disposed on the first substrate side, and a second metal laminated on the first metal layer and different from the first metal. You may have the 2nd metal layer which consists of.

材料特性の異なる第一の金属と第二の金属とを積層することによって、耐熱性、耐食性等の異なる二つの材料特性を同時に達成できる中空構造部材を製造することが可能となる。   By laminating the first metal and the second metal having different material characteristics, it is possible to manufacture a hollow structural member that can simultaneously achieve two material characteristics such as heat resistance and corrosion resistance.

さらに、本発明に係る燃焼器は、筒状燃焼室と、該筒状燃焼室の中心に配置されて前記筒状燃焼室内へ燃料を送り込むバーナとを有する燃焼器であって、前記筒状燃焼室が、上記の製造方法によって製造された中空構造部材によって形成されてなることを特徴とする。   Furthermore, the combustor according to the present invention is a combustor having a cylindrical combustion chamber and a burner that is arranged at the center of the cylindrical combustion chamber and feeds fuel into the cylindrical combustion chamber. The chamber is formed by a hollow structural member manufactured by the above manufacturing method.

このような燃焼器においては、筒状燃焼室に用いられる中空構造部材を製造工程の短縮を図りながら製造することができる。また、この中空構造部材に延性等の低下がなく、この結果、中空構造部材から容易に筒状燃焼室を製造することができる。   In such a combustor, the hollow structural member used for the cylindrical combustion chamber can be manufactured while shortening the manufacturing process. Further, the hollow structure member does not have a decrease in ductility and the like, and as a result, the cylindrical combustion chamber can be easily manufactured from the hollow structure member.

本発明に係る中空構造部材の製造方法、及び中空構造部材を備えた燃焼器によると、中空構造部材の製造において、屈曲板の設置工程と金属溶射を用いた溶射工程とを備えることによって、製造時間短縮と加工性の向上とを達成することが可能となる。   According to the method for manufacturing a hollow structural member according to the present invention and the combustor including the hollow structural member, the manufacturing of the hollow structural member includes the step of installing a bent plate and the thermal spraying process using metal spraying. It is possible to achieve a reduction in time and an improvement in workability.

ガスタービン燃焼器の近傍を模式的に示す図である。It is a figure which shows typically the vicinity of a gas turbine combustor. 本発明の第一実施形態に係る燃焼室内筒を拡大して模式的に示す図である。It is a figure which expands and shows typically a combustion chamber cylinder concerning a first embodiment of the present invention. 本発明の第一実施形態に係る燃焼室内筒の製造方法の手順を示すフロー図である。It is a flowchart which shows the procedure of the manufacturing method of the combustion chamber cylinder which concerns on 1st embodiment of this invention. 本発明の第一実施形態に係る燃焼室内筒の製造方法の手順を示す模式図である。It is a schematic diagram which shows the procedure of the manufacturing method of the combustion chamber cylinder which concerns on 1st embodiment of this invention. 本発明の第二実施形態に係る燃焼室内筒の製造方法の手順を示すフロー図である。It is a flowchart which shows the procedure of the manufacturing method of the combustion chamber cylinder which concerns on 2nd embodiment of this invention. 本発明の第二実施形態に係る燃焼室内筒の製造方法の手順を示す模式図である。It is a schematic diagram which shows the procedure of the manufacturing method of the combustion chamber cylinder which concerns on 2nd embodiment of this invention. 本発明の第三実施形態に係る燃焼室内筒の製造方法の手順を示すフロー図である。It is a flowchart which shows the procedure of the manufacturing method of the combustion chamber cylinder which concerns on 3rd embodiment of this invention. 本発明の第三実施形態に係る燃焼室内筒の製造方法の手順を示す模式図である。It is a schematic diagram which shows the procedure of the manufacturing method of the combustion chamber cylinder which concerns on 3rd embodiment of this invention. 本発明の第四実施形態に係る燃焼室内筒に用いられる中空構造部材を示す図である。It is a figure which shows the hollow structure member used for the combustion chamber cylinder which concerns on 4th embodiment of this invention.

以下、本発明の第一実施形態に係る燃焼室内筒(筒状燃焼室)1(以下、単に内筒1と称する)の製造方法について説明する。
本実施形態において製造される内筒1は、図1及び図2に示すように、ガスタービン燃焼器100における燃焼室90の内壁面を形成する筒状部材である。
このようなガスタービン燃焼器100は、バーナ2より燃焼室90に燃料が流入し、燃焼されることによって高温の燃焼ガスWが生成されるように構成されている。この燃焼ガスWは尾筒3を通じて図示しないタービンへ送り込まれ、回転動力に変換されるようになっている。
Hereinafter, a method for manufacturing a combustion chamber cylinder (cylindrical combustion chamber) 1 (hereinafter simply referred to as an inner cylinder 1) according to the first embodiment of the present invention will be described.
The inner cylinder 1 manufactured in the present embodiment is a cylindrical member that forms the inner wall surface of the combustion chamber 90 in the gas turbine combustor 100 as shown in FIGS. 1 and 2.
Such a gas turbine combustor 100 is configured such that fuel flows from the burner 2 into the combustion chamber 90 and is combusted to generate a high-temperature combustion gas W. This combustion gas W is sent to a turbine (not shown) through the transition piece 3 and converted into rotational power.

このように内筒1においては、高温の燃焼ガスWが生成されるため、ガスタービン運転時には内筒1の内部は常時高温状態に曝される。従って、内筒1は、耐熱性及び耐食性に優れた例えば、インコネル等の金属材料を用いて製造される。また、内筒1の内面1aと外面1bとの間には軸線P方向の一方側から他方側に貫通する複数の冷却孔(中空孔)4が設けられており、この冷却孔4に冷却空気が流通することによって、冷却空気との間で熱交換を行い、内筒1の冷却が行なわれるようになっている。   Thus, in the inner cylinder 1, since the high temperature combustion gas W is produced | generated, the inside of the inner cylinder 1 is always exposed to a high temperature state at the time of gas turbine operation. Therefore, the inner cylinder 1 is manufactured using a metal material such as Inconel, which is excellent in heat resistance and corrosion resistance. A plurality of cooling holes (hollow holes) 4 penetrating from one side of the axis P direction to the other side are provided between the inner surface 1 a and the outer surface 1 b of the inner cylinder 1, and cooling air is provided in the cooling holes 4. Circulates, heat exchange is performed with the cooling air, and the inner cylinder 1 is cooled.

次に図3に示すフロー図に沿って、内筒1の製造方法の手順について説明する。
内筒1の製造方法は、屈曲板設置準備工程S1と、屈曲板設置工程(設置工程)S2と、金属溶射工程(溶射工程)S3と、筒状化工程S4とを備えている。
Next, the procedure of the manufacturing method of the inner cylinder 1 will be described along the flowchart shown in FIG.
The manufacturing method of the inner cylinder 1 includes a bent plate installation preparation step S1, a bent plate installation step (installation step) S2, a metal spraying step (spraying step) S3, and a cylindrical forming step S4.

まず、図4(a)に示すように屈曲板設置準備工程S1を実行する。即ち、インコネル等の金属材料よりなる板材から、内筒1の直径と同じ長さの矩形状部材をシャーリング加工等によって切り出す。そしてプレス加工等によってこの矩形状部材に屈曲凹面10aを形成して、一方側を向く面を湾曲させることによって屈曲板10を製造する。なお、この屈曲板10の屈曲凹面10aは、冷却空気の流通する流路となる。   First, as shown in FIG. 4A, the bending plate installation preparation step S1 is executed. That is, a rectangular member having the same length as the diameter of the inner cylinder 1 is cut out from a plate material made of a metal material such as Inconel by shearing or the like. The bending plate 10 is manufactured by forming the bending concave surface 10a on the rectangular member by pressing or the like and curving the surface facing one side. The bent concave surface 10a of the bent plate 10 serves as a flow path through which cooling air flows.

そして、この屈曲板10を、屈曲凹面10aを上方に向けた状態で型21の上に載置する。この際、各屈曲板10の長手方向を同一方向に向けた状態で等間隔に各屈曲板10を配置する。なお、この型21には屈曲板10の屈曲凹面10aの反対側の屈曲凸面10bにちょうど一致するように溝部21aが形成されており、屈曲板10を載置した際にはこの屈曲板10が収容されるようになっている。   The bending plate 10 is placed on the mold 21 with the bending concave surface 10a facing upward. At this time, the bending plates 10 are arranged at equal intervals in a state where the longitudinal directions of the bending plates 10 are directed in the same direction. The mold 21 has a groove 21a formed so as to coincide with the bending convex surface 10b opposite to the bending concave surface 10a of the bending plate 10. When the bending plate 10 is placed, the bending plate 10 is It is to be accommodated.

続いて、図4(b)に示すように屈曲板設置工程S2、即ち、インコネル等の金属材料よりなる薄板(第一基板)22を、屈曲板10を載置した型21の上方から覆うように配置し、スポット溶接によって屈曲板10とこの薄板22との仮接合を行ない、屈曲板10を薄板22上に固定する。なお、この薄板22における屈曲板10が接合される面と反対側の面は、最終的に内筒1の内面1a又は外面1bとなるものである。   Subsequently, as shown in FIG. 4B, the bending plate installation step S2, that is, the thin plate (first substrate) 22 made of a metal material such as Inconel is covered from above the mold 21 on which the bending plate 10 is placed. The bent plate 10 and the thin plate 22 are temporarily joined by spot welding, and the bent plate 10 is fixed on the thin plate 22. The surface of the thin plate 22 opposite to the surface to which the bent plate 10 is joined finally becomes the inner surface 1a or the outer surface 1b of the inner cylinder 1.

さらに、図4(c)、図4(d)及び図4(e)に示すように、金属溶射工程S3を実行する。即ち、屈曲板10が仮接合された薄板22を型21から取り外し、上下逆向きに転換して載置する。そして、薄板22における屈曲板10が接合された面側へインコネル等からなる溶融金属Mの溶射を行い、屈曲板10の屈曲凸面10bによって薄板22上に形成された凸凹を無くすように、平面(第二基板)23を形成するスプレイフォーミングを行なう。このようにして形成された上記平面23は、最終的に内筒1の内面1a又は外面1bとなるものである。このようにして中空構造、即ち、複数の冷却孔4を有する中空構造部材20が製造される。   Further, as shown in FIGS. 4C, 4D, and 4E, a metal spraying step S3 is performed. That is, the thin plate 22 to which the bending plate 10 is temporarily joined is removed from the mold 21 and placed in the upside down direction. And the molten metal M which consists of inconel etc. is sprayed to the surface side in which the bending board 10 in the thin board 22 was joined, and a flat surface (so that the unevenness formed on the thin board 22 by the bending convex surface 10b of the bending board 10 is eliminated. Spray forming for forming the second substrate 23 is performed. The flat surface 23 formed in this way finally becomes the inner surface 1a or the outer surface 1b of the inner cylinder 1. Thus, a hollow structure, that is, a hollow structure member 20 having a plurality of cooling holes 4 is manufactured.

最後に、図4(f)に示すように筒状化工程S4を実行する。即ち、上記中空構造部材20がプレス加工等を用いて円筒状に曲げ加工され、中空構造部材20の端縁20a同士を溶接によって接合する。このようにして、円筒の内面1aと外面1bとの間に中空構造、即ち、複数の冷却孔4が形成され、この冷却孔4に冷却空気が流通可能な内筒1が製造される。   Finally, as shown in FIG. 4F, the cylindrical step S4 is performed. That is, the hollow structural member 20 is bent into a cylindrical shape using a press process or the like, and the edges 20a of the hollow structural member 20 are joined together by welding. In this way, a hollow structure, that is, a plurality of cooling holes 4 is formed between the inner surface 1a and the outer surface 1b of the cylinder, and the inner cylinder 1 through which cooling air can flow is manufactured.

以上のような内筒1の製造方法によれば、屈曲板10と薄板22とを仮接合した後に金属溶射工程S3を実行することによって、中空構造部材20を製造することができる。従って、放電加工や機械加工等を用いて冷却孔4を形成する工程や、ロウ付け等によって複数の板を張り合わせるといった工程は不要であり、中空構造部材20製造の工程を短縮することができる。   According to the manufacturing method of the inner cylinder 1 as described above, the hollow structure member 20 can be manufactured by performing the metal spraying step S3 after temporarily joining the bent plate 10 and the thin plate 22. Therefore, the process of forming the cooling hole 4 using electric discharge machining, machining, or the like, or the process of bonding a plurality of plates by brazing or the like is unnecessary, and the process of manufacturing the hollow structural member 20 can be shortened. .

さらに、ロウ付け材料による張り合わせを行なわず、金属溶射工程S3によって一体成形を行うため、筒状化工程S4においてプレス加工を実行した際にも、このロウ付け材料によって中空構造部材20の延性が低下することを防ぎ、ロウ付け材料を起因とした中空構造部材20の割れの発生を防止することができる。従って、中空構造部材20の加工性の向上を図ることができ、様々な形状に加工可能となる。   Further, since the single molding is performed by the metal spraying step S3 without performing the bonding with the brazing material, the ductility of the hollow structural member 20 is reduced by the brazing material even when the press working is performed in the cylindrical forming step S4. It is possible to prevent the occurrence of cracks in the hollow structural member 20 due to the brazing material. Therefore, the workability of the hollow structural member 20 can be improved and can be processed into various shapes.

ここで、溶射によって金属製品を形成するスプレイフォーミングとは、溶融金属Mを細いノズルから噴射し、高圧の、例えば窒素ガス等の不活性ガスを噴き付けることによって、溶融金属Mを微細な霧状の液滴、即ち、半溶融半凝固状態としてテーブル上に降り積もらせて、金属製品を形成する手法である。なお、溶射中にテーブルの形状やテーブルの動きを変化させることによって、この金属製品の形状を様々に選択することができる   Here, spray forming in which a metal product is formed by thermal spraying is a method in which the molten metal M is sprayed from a thin nozzle, and a high-pressure inert gas such as nitrogen gas is sprayed to form the molten metal M in a fine mist form. In this method, the metal product is formed by being dropped on the table in a semi-molten and semi-solid state. In addition, the shape of this metal product can be selected variously by changing the shape of the table and the movement of the table during thermal spraying.

また、上記スプレイフォーミングにおいては、テーブル上に降り積もる間に溶融金属Mが急冷凝固し、金属製品が形成される。従って、金属組織の偏析がなく均一化できること、及び、組織の微細化を図ることが可能であり、金属製品の強度向上につながる。また、合金材料よりなる金属製品を製造する際には、合金元素を高濃度に含有させることが可能となり、より強度の高い合金材料よりなる金属製品を製造することもできる。   In the spray forming, the molten metal M rapidly cools and solidifies while falling on the table to form a metal product. Therefore, the metal structure can be made uniform without segregation, and the structure can be made finer, which leads to an improvement in the strength of the metal product. Moreover, when manufacturing the metal product which consists of alloy materials, it becomes possible to contain an alloy element in high concentration, and the metal product which consists of alloy materials with higher intensity | strength can also be manufactured.

本実施形態の内筒1の製造方法によれば、屈曲板10を設置した状態で金属溶射工程S3を実行することによって、工程短縮による製造時間短縮が可能となり、コストダウンも達成できる。また、中空構造部材20の加工性を向上でき、目的とする形状の内筒1を容易に確実に形成することができる。   According to the manufacturing method of the inner cylinder 1 of the present embodiment, by performing the metal spraying step S3 with the bent plate 10 installed, the manufacturing time can be shortened by shortening the process, and the cost can be reduced. Moreover, the workability of the hollow structural member 20 can be improved, and the inner cylinder 1 having a target shape can be easily and reliably formed.

さらに、スプレイフォーミングを用いた金属溶射工程S3によって、内筒1の材料となる中空構造部材20の強度向上を達成でき、また、中空構造部材20の形状、材質、板厚の選択も容易となるため、容易かつ確実に中空構造部材20を製造することができる。   Furthermore, the metal spraying step S3 using spray forming can achieve improvement in the strength of the hollow structural member 20 that is the material of the inner cylinder 1, and the shape, material, and plate thickness of the hollow structural member 20 can be easily selected. Therefore, the hollow structural member 20 can be manufactured easily and reliably.

次に、図5のフロー図に沿って、第二実施形態に係る内筒1の製造方法について説明する。
なお、第一実施形態と同様の構成要素には同一の符号を付して詳細説明を省略する。
内筒1の製造方法は、セラミックコア設置工程(設置工程)S10と、金属溶射工程(溶射工程)S3と、溶解工程S11と、筒状化工程S4とを備えている。即ち、第二実施形態は、屈曲板設置準備工程S1及び屈曲板設置工程S2に代えてセラミックコア設置工程S10を備えている点で第一実施形態とは異なっている。
Next, the manufacturing method of the inner cylinder 1 which concerns on 2nd embodiment is demonstrated along the flowchart of FIG.
In addition, the same code | symbol is attached | subjected to the component similar to 1st embodiment, and detailed description is abbreviate | omitted.
The manufacturing method of the inner cylinder 1 includes a ceramic core installation step (installation step) S10, a metal spraying step (spraying step) S3, a melting step S11, and a cylindrical forming step S4. That is, the second embodiment is different from the first embodiment in that a ceramic core installation step S10 is provided instead of the bending plate installation preparation step S1 and the bending plate installation step S2.

まず、図6(a)に示すようにセラミックコア設置工程S10を実行する。即ち、インコネル等の金属材料よりなる薄板22の上に、セラミック材料である例えば、シリカ、ムライト、アルミナ等からなる棒部材であるセラミックコア30を複数、その延在方向を同一方向に向けた状態で等間隔に載置する。なおこの薄板22においてセラミックコア30が載置される面と反対側の面は最終的に内筒1の内面1a又は外面1bとなるものである。なお、セラミックコア30は、上記屈曲板10と同じ形状であってもよいし、丸棒であってもよく、断面形状は限定されない。なお、このセラミックコア30の占める空間は、最終的に冷却空気の流通する流路空間となる。   First, as shown in FIG. 6A, a ceramic core installation step S10 is performed. That is, on a thin plate 22 made of a metal material such as Inconel, a plurality of ceramic cores 30 that are rod members made of, for example, silica, mullite, alumina, etc., which are ceramic materials, with their extending directions oriented in the same direction Place them at regular intervals. Note that the surface of the thin plate 22 opposite to the surface on which the ceramic core 30 is placed finally becomes the inner surface 1 a or the outer surface 1 b of the inner cylinder 1. The ceramic core 30 may have the same shape as the bent plate 10 or a round bar, and the cross-sectional shape is not limited. The space occupied by the ceramic core 30 finally becomes a flow path space through which cooling air flows.

次に、図6(b)に示すように金属溶射工程S3を実行する。この金属溶射工程S3には第一実施形態と同様にスプレイフォーミングが用いられる。即ち、複数のセラミックコア30が載置された薄板22の上方よりインコネル等からなる溶融金属Mの溶射を行い、セラミックコア30によって薄板22上に形成された凸凹を無くすように、平面23を形成するスプレイフォーミングを行なう。このようにして形成された平面23は、最終的に内筒1の内面1aもしくは外面1bとなるものである。こうして内部にセラミックコア30が埋め込まれた板材31が形成される。   Next, as shown in FIG. 6B, a metal spraying step S3 is performed. In this metal spraying step S3, spray forming is used as in the first embodiment. That is, the molten metal M made of inconel or the like is sprayed from above the thin plate 22 on which the plurality of ceramic cores 30 are placed, and the flat surface 23 is formed so as to eliminate the unevenness formed on the thin plate 22 by the ceramic core 30. Perform spray forming. The flat surface 23 thus formed finally becomes the inner surface 1a or the outer surface 1b of the inner cylinder 1. In this way, a plate 31 having the ceramic core 30 embedded therein is formed.

続いて、図6(c)及び図6(d)に示すように溶解工程S11を実行する。即ち、セラミックコア設置工程S10及び金属溶射工程S3を実行することによって、板材31の内部に埋め込まれた状態となったセラミックコア30を例えば、水酸化ナトリウム、水酸化カリウム等のアルカリ溶液によって溶解し、上記板材31にセラミックコア30の外形と同じ内周面を有する冷却孔4を形成し、複数の冷却孔4を有する中空構造部材20が製造される。   Subsequently, as shown in FIGS. 6C and 6D, the melting step S11 is performed. That is, by executing the ceramic core installation step S10 and the metal spraying step S3, the ceramic core 30 embedded in the plate 31 is dissolved by an alkaline solution such as sodium hydroxide or potassium hydroxide. The cooling hole 4 having the same inner peripheral surface as the outer shape of the ceramic core 30 is formed in the plate material 31, and the hollow structure member 20 having the plurality of cooling holes 4 is manufactured.

最後に、図6(e)に示すように筒状化工程S4を実行する。この筒状化工程S4は、第一実施形態と同一の工程であり、即ち、上記中空構造部材20がプレス加工等を用いて円筒状に曲げ加工され、中空構造部材20の端縁20a同士を溶接によって接合する。このようにして、円筒の内面1aと外面1bとの間に中空構造、即ち、複数の冷却孔4が形成され、この冷却孔4に冷却空気が流通可能な内筒1が製造される。   Finally, as shown in FIG. 6E, the cylindrical step S4 is performed. This cylindrical process S4 is the same process as the first embodiment, that is, the hollow structural member 20 is bent into a cylindrical shape using a press process or the like, and the edges 20a of the hollow structural member 20 are joined together. Join by welding. In this way, a hollow structure, that is, a plurality of cooling holes 4 is formed between the inner surface 1a and the outer surface 1b of the cylinder, and the inner cylinder 1 through which cooling air can flow is manufactured.

以上のような内筒1の製造方法によれば、セラミックコア30を薄板22に載置した後に金属溶射工程S3を施すことによって、中空構造部材20を製造することができる。従って、放電加工や機械加工等を用いて冷却孔4を形成する工程や、ロウ付け等によって複数の板を張り合わせる工程は不要であり、さらに、第一実施形態の屈曲板設置準備工程S1のように、型21に屈曲板10を設置する作業等が不要であるため、中空構造部材20の製造までの工程をさらに短縮することができる。   According to the manufacturing method of the inner cylinder 1 as described above, the hollow structure member 20 can be manufactured by performing the metal spraying step S3 after placing the ceramic core 30 on the thin plate 22. Therefore, the step of forming the cooling holes 4 using electric discharge machining, machining, or the like, or the step of bonding a plurality of plates by brazing or the like is unnecessary, and further, the bending plate installation preparation step S1 of the first embodiment is not necessary. Thus, since the operation | work etc. which install the bending board 10 in the type | mold 21 are unnecessary, the process until manufacture of the hollow structure member 20 can further be shortened.

さらに、ロウ付け材料による張り合わせを行なわず、金属溶射工程S3によって一体成形を行うため、筒状化工程S4においてプレス加工を施工した際にも、このロウ付け材料によって中空構造部材20の延性が低下による中空構造部材20の割れを防止することができ、加工性の向上を図ることができる。   Further, since the single molding is performed by the metal spraying step S3 without performing the bonding with the brazing material, the ductility of the hollow structural member 20 is reduced by this brazing material even when the press working is performed in the cylindrical forming step S4. It is possible to prevent the hollow structural member 20 from being cracked, and to improve workability.

また、スプレイフォーミングを用いた金属溶射工程S3によって、中空構造部材20の強度を向上でき、中空構造部材20の材料、形状、板厚等も容易に変更することができる。   Further, the strength of the hollow structural member 20 can be improved by the metal spraying step S3 using spray forming, and the material, shape, plate thickness, etc. of the hollow structural member 20 can be easily changed.

さらに、セラミックコア30の形状を様々に変更することによって、冷却孔4の形状を様々に選択することが容易である。例えば、冷却空気の流路形状や、流路内径を流路方向に変化させる場合には、延在方向に徐々に形状や径の変化するセラミックコア30を用いることによって、複雑な流路を形成できる。   Furthermore, it is easy to select various shapes of the cooling holes 4 by changing the shape of the ceramic core 30 in various ways. For example, when changing the flow path shape of the cooling air or the flow path inner diameter in the flow path direction, a complex flow path is formed by using the ceramic core 30 whose shape and diameter gradually change in the extending direction. it can.

本実施形態の内筒1の製造方法によれば、セラミックコア30を薄板22上に載置した状態で金属溶射工程S3を実行することによって、工程の短縮による製造時間短縮が可能となる。従って、コストダウンも達成できる。また、中空構造部材20の加工性を向上でき、目的とする形状の内筒1を容易に確実に形成することができる。   According to the manufacturing method of the inner cylinder 1 of the present embodiment, by performing the metal spraying step S3 in a state where the ceramic core 30 is placed on the thin plate 22, the manufacturing time can be reduced by shortening the steps. Therefore, cost reduction can also be achieved. Moreover, the workability of the hollow structural member 20 can be improved, and the inner cylinder 1 having a target shape can be easily and reliably formed.

さらに、スプレイフォーミングの金属溶射工程S3によって、内筒1の材料となる中空構造部材20の強度向上及び材質、形状、板厚の選択も容易となり、製造目的とする内筒1に合わせて、容易かつ確実に中空構造部材20を製造することができる。また、セラミックコア30の形状変更によって、必要とする冷却効果を得られるように、様々な形状の冷却孔4を容易に形成できる。   Furthermore, the spray forming metal spraying step S3 makes it easy to improve the strength of the hollow structural member 20 that is the material of the inner cylinder 1 and to select the material, shape, and plate thickness. And the hollow structure member 20 can be manufactured reliably. Moreover, the cooling holes 4 having various shapes can be easily formed so that the required cooling effect can be obtained by changing the shape of the ceramic core 30.

次に、図7に示すフロー図に沿って、第三実施形態に係る内筒1の製造方法について説明する。
なお、第一実施形態及び第二実施形態と同様の構成要素には同一の符号を付して詳細説明を省略する。
内筒1の製造方法は、第一実施形態同様に屈曲板設置準備工程S1と、屈曲板設置工程(設置工程)S2と、金属溶射工程(溶射工程)S3とを備えている。即ち、第三実施形態は、筒状化工程S4を備えていない点で第一実施形態とは異なっている。
Next, the manufacturing method of the inner cylinder 1 according to the third embodiment will be described along the flowchart shown in FIG.
In addition, the same code | symbol is attached | subjected to the component similar to 1st embodiment and 2nd embodiment, and detailed description is abbreviate | omitted.
The manufacturing method of the inner cylinder 1 includes a bent plate installation preparation step S1, a bent plate installation step (installation step) S2, and a metal spraying step (spraying step) S3 as in the first embodiment. That is, the third embodiment is different from the first embodiment in that the cylindrical step S4 is not provided.

まず、図8(a)に示すように屈曲板設置準備工程S1、及び屈曲板設置工程S2を実行する。ここで、第一実施形態の屈曲板設置準備工程S1、及び、屈曲板設置工程S2においては、屈曲板10を薄板22上に仮接合して設置しているが、本実施形態では、薄板22に代えて円筒部材(第一基板)40の外周面上に屈曲板10をスポット溶接によって仮接合して設置する。なお、この円筒部材40における屈曲板10が接合される面と反対側の面は最終的に内筒1の内面1aとなるものである。   First, as shown in FIG. 8A, the bending plate installation preparation step S1 and the bending plate installation step S2 are executed. Here, in the bending plate installation preparation step S1 and the bending plate installation step S2 of the first embodiment, the bending plate 10 is temporarily joined and installed on the thin plate 22, but in this embodiment, the thin plate 22 is installed. Instead, the bent plate 10 is temporarily bonded on the outer peripheral surface of the cylindrical member (first substrate) 40 by spot welding. Note that the surface of the cylindrical member 40 opposite to the surface to which the bent plate 10 is joined finally becomes the inner surface 1 a of the inner cylinder 1.

さらに、図8(b)に示すように、金属溶射工程S3を実行する。この金属溶射工程S3は第一実施形態と同様にスプレイフォーミングが用いられる。即ち、円筒部材40における屈曲板10が接合された面側に溶融金属Mの溶射を行い、屈曲板10の屈曲凸面10bによって円筒部材40の外周面上に形成された凸凹を無くすように円筒外面(第二基板)41を形成するスプレイフォーミングを行なう。このようにして形成された円筒外面41は、最終的に内筒1の外面1bとなるものである。このようにして内部に中空構造、即ち、複数の冷却孔4を有する内筒1が製造される。   Further, as shown in FIG. 8B, a metal spraying step S3 is performed. In this metal spraying step S3, spray forming is used as in the first embodiment. That is, the outer surface of the cylindrical member 40 is sprayed with the molten metal M on the surface side of the cylindrical member 40 to which the bent plate 10 is joined, and the unevenness formed on the outer peripheral surface of the cylindrical member 40 by the bent convex surface 10b of the bent plate 10 is eliminated. (Second substrate) 41 is formed by spray forming. The cylindrical outer surface 41 thus formed finally becomes the outer surface 1b of the inner cylinder 1. In this way, the hollow cylinder, that is, the inner cylinder 1 having a plurality of cooling holes 4 is manufactured.

以上のような内筒1の製造方法によれば、屈曲板10と円筒部材40とを仮接合した後に金属溶射工程S3によって、直接内筒1を製造することができる。従って、放電加工や機械加工等を用いて冷却孔4を形成する工程や、ロウ付け等によって複数の板を張り合わせるといった工程は不要であり、製造までの工程を短縮することができる。   According to the manufacturing method of the inner cylinder 1 as described above, the inner cylinder 1 can be directly manufactured by the metal spraying step S3 after the bending plate 10 and the cylindrical member 40 are temporarily joined. Therefore, the process of forming the cooling holes 4 using electric discharge machining, machining, or the like, or the process of pasting together a plurality of plates by brazing or the like is unnecessary, and the process up to manufacture can be shortened.

さらに、ロウ付け材料による張り合わせを行なわず、金属溶射工程S3によって一体成形を行うため、ロウ付け材料を起因とした割れの発生を防止することができる。即ち、加工性の向上を図ることができ、様々な形状に加工可能となる。   Further, since the integral molding is performed by the metal spraying step S3 without performing the bonding with the brazing material, it is possible to prevent the occurrence of cracks due to the brazing material. In other words, the workability can be improved, and various shapes can be processed.

そして、このようなスプレイフォーミングを用いた金属溶射工程S3によって材料、形状、板厚等も容易に選択することができる。   The material, shape, thickness, etc. can be easily selected by the metal spraying step S3 using such spray forming.

また、第一実施形態、及び、第二実施形態のように中空構造部材20を製造した後に、この中空構造部材20をプレス加工して円筒形状に形成する必要がないため、高強度材料であり、プレス加工が困難であるような、例えば、析出強化型21ニッケル基合金を用いて内筒1を製造することもできる。   In addition, since the hollow structural member 20 is manufactured as in the first embodiment and the second embodiment, it is not necessary to press the hollow structural member 20 to form a cylindrical shape. The inner cylinder 1 can also be manufactured using, for example, a precipitation-strengthened 21 nickel-base alloy that is difficult to press.

本実施形態の内筒1の製造方法によれば、屈曲板10を円筒部材40に設置した状態で金属溶射を行なうことによって、工程の短縮による製造時間短縮が可能となり、コストダウンも達成できる。また、加工性を向上でき、目的とする形状の内筒1を容易に確実に形成することが可能となる。   According to the manufacturing method of the inner cylinder 1 of the present embodiment, by performing metal spraying in a state where the bending plate 10 is installed on the cylindrical member 40, the manufacturing time can be shortened by shortening the process, and the cost can be reduced. Moreover, workability can be improved and the inner cylinder 1 having a desired shape can be easily and reliably formed.

そして、スプレイフォーミングを用いた金属溶射工程S3によって、内筒1の強度向上の達成ができ、また、内筒1の材質、形状、板厚の選択も容易となる。
さらに、中空構造部材20を経由せずにスプレイフォーミングによって直接内筒1を製造できるため、耐熱性、耐食性の高い高強度材料を用いることができ、燃焼器100の性能向上につながる。
The strength of the inner cylinder 1 can be improved by the metal spraying step S3 using spray forming, and the material, shape, and plate thickness of the inner cylinder 1 can be easily selected.
Furthermore, since the inner cylinder 1 can be directly manufactured by spray forming without going through the hollow structural member 20, a high-strength material having high heat resistance and corrosion resistance can be used, which leads to improvement in the performance of the combustor 100.

ここで、本実施形態では屈曲板10を円筒部材40に仮接合した状態で、金属溶射を行なうことによって内筒1を製造したが、第二実施形態同様に、屈曲板設置準備工程S1と、屈曲板設置工程S2とに代えて、セラミックコア30設置工程S10を採用してもよい。即ち、円筒部材40にセラミックコア30を載置した状態で、スプレイフォーミングを用いた金属溶射工程S3を実行し、溶解工程S11によってセラミックコア30を溶解して、複数の冷却孔4が形成された内筒1を製造してもよい。この場合、内筒1の製造までの工程をさらに短縮できる。   Here, in the present embodiment, the inner cylinder 1 is manufactured by performing metal spraying in a state where the bending plate 10 is temporarily joined to the cylindrical member 40. However, similarly to the second embodiment, the bending plate installation preparation step S1; Instead of the bending plate installation step S2, a ceramic core 30 installation step S10 may be adopted. That is, in a state where the ceramic core 30 is placed on the cylindrical member 40, the metal spraying step S3 using spray forming is executed, and the ceramic core 30 is melted by the melting step S11, and a plurality of cooling holes 4 are formed. The inner cylinder 1 may be manufactured. In this case, the process up to the production of the inner cylinder 1 can be further shortened.

次に、第四実施形態に係る内筒1の製造方法について説明する。
内筒1の製造方法は、第一実施形態同様に屈曲板設置準備工程S1と、屈曲板設置工程S2(設置工程)と、金属溶射工程S3(溶射工程)と、筒状化工程S4とを備えている。なお、第四実施形態は、金属溶射工程S3において用いる溶融金属Mが異なっている点で、第一実施形態と異なっている。
Next, a method for manufacturing the inner cylinder 1 according to the fourth embodiment will be described.
As with the first embodiment, the manufacturing method of the inner cylinder 1 includes a bent plate installation preparation step S1, a bent plate installation step S2 (installation step), a metal spraying step S3 (spraying step), and a cylindrical forming step S4. I have. The fourth embodiment is different from the first embodiment in that the molten metal M used in the metal spraying step S3 is different.

まず、第一実施形態同様に屈曲板設置準備工程S1、及び屈曲板設置工程S2を実行する。
続いて、金属溶射工程S3を実行する。この金属溶射工程S3は第一実施形態と同様にスプレイフォーミングが用いられる。即ち、複数の屈曲板10が接合された薄板(第一基板)22上に溶融金属Mの溶射を行い、屈曲板10の屈曲凸面10bによって薄板22上に形成された凸凹を無くすように平面(第二基板)23を形成するスプレイフォーミングを行なう。このとき、用いる溶融金属Mは、まず初めに延性に優れた例えば、トミロイ、インコネル617、Nimonic263等の第一の金属50を溶射する。続いて、この第一の金属50の表面を覆うように、耐熱性及び耐食性に優れた例えば、ヘインズ214、ヘインズ230、インコネル693等の第二の金属51を溶射し、第一の金属50と第二の金属51の二層構造とした中空構造部材20を製造する。
First, similarly to the first embodiment, the bending plate installation preparation step S1 and the bending plate installation step S2 are executed.
Subsequently, the metal spraying step S3 is performed. In this metal spraying step S3, spray forming is used as in the first embodiment. That is, the molten metal M is thermally sprayed on the thin plate (first substrate) 22 to which the plurality of bent plates 10 are joined, and a flat surface is formed so that the unevenness formed on the thin plate 22 by the bent convex surface 10b of the bent plate 10 is eliminated. Spray forming for forming the second substrate 23 is performed. At this time, the molten metal M to be used is first sprayed with a first metal 50 having excellent ductility, such as Tomiloy, Inconel 617, and Nimonic 263. Subsequently, a second metal 51 such as Haynes 214, Haynes 230, Inconel 693 or the like excellent in heat resistance and corrosion resistance is sprayed so as to cover the surface of the first metal 50, and the first metal 50 and The hollow structural member 20 having a two-layer structure of the second metal 51 is manufactured.

次に、第一実施形態同様に筒状化工程S4を実行する。即ち、上記中空構造部材20がプレス加工等を用いて円筒状に形成され中空構造部材20の端縁20a同士を溶接によって接合する。この際、第二の金属51側が円筒の内面1aとなるように筒状化を行なう。このようにして、円筒の内面1aと外面1bとの間に中空構造、即ち、複数の冷却孔4が形成され、冷却孔4に冷却空気が流通可能な内筒1が製造される。   Next, the cylindrical step S4 is executed as in the first embodiment. That is, the hollow structural member 20 is formed into a cylindrical shape using press working or the like, and the edges 20a of the hollow structural member 20 are joined together by welding. At this time, the cylinder is formed so that the second metal 51 side becomes the inner surface 1a of the cylinder. In this manner, a hollow structure, that is, a plurality of cooling holes 4 is formed between the inner surface 1 a and the outer surface 1 b of the cylinder, and the inner cylinder 1 through which the cooling air can flow is manufactured.

以上のような内筒1の製造方法によれば、冷却孔4を形成する工程や、ロウ付け等によって複数の板を張り合わせるといった工程は不要であり、中空構造部材20の製造までの工程を短縮することができる。   According to the manufacturing method of the inner cylinder 1 as described above, the process of forming the cooling holes 4 and the process of pasting together a plurality of plates by brazing or the like are unnecessary, and the process up to the manufacture of the hollow structural member 20 is performed. It can be shortened.

また、ロウ付け材料による張り合わせを行なわず、金属溶射工程S3によって一体成形を行うため、筒状化工程S4においてプレス加工を施工した際にも、このロウ付け材料によって中空構造部材20の延性が低下し、ロウ付け材料を起因とした中空構造部材20の割れの発生を防止することができ、加工性の向上を図ることができる。   In addition, since the molding is performed by the metal spraying step S3 without performing the bonding with the brazing material, the ductility of the hollow structural member 20 is lowered by the brazing material even when the press working is performed in the cylindrical forming step S4. In addition, it is possible to prevent the hollow structure member 20 from being cracked due to the brazing material, and to improve workability.

そして、スプレイフォーミングを用いた金属溶射工程S3によって、中空構造部材20の強度を向上でき、中空構造部材20の材料、形状、板厚等も容易に選択することができる。   The strength of the hollow structural member 20 can be improved by the metal spraying process S3 using spray forming, and the material, shape, plate thickness, etc. of the hollow structural member 20 can be easily selected.

さらに、第一の金属50と第二の金属51の二層構造を有することで、筒状化工程S4のプレス加工時にも第一の金属50によって延性をさらに向上し割れを防止するとともに、第二の金属51によって高温環境に曝される内筒1内面1aの耐熱性、耐食性の向上も達成できる。   Furthermore, by having a two-layer structure of the first metal 50 and the second metal 51, the ductility is further improved by the first metal 50 even during the press working in the cylindrical step S4, and cracking is prevented. Improvement in heat resistance and corrosion resistance of the inner surface 1a of the inner cylinder 1 exposed to the high temperature environment by the second metal 51 can also be achieved.

本実施形態の内筒1の製造方法によれば、屈曲板10を設置した状態で金属溶射工程S3を実行することによって、工程の短縮による製造時間短縮が可能となる。そして、スプレイフォーミングを用いた金属溶射工程S3によって、内筒1の強度向上が達成でき、また、内筒1の材質、形状、板厚の選択も容易となる。さらに、中空構造部材20に二層構造を採用することによって、中空構造部材20の加工性の向上と、耐熱性及び耐食性の向上とを同時に達成でき、内筒1の製造の容易化と性能向上とを同時に達成できる。   According to the manufacturing method of the inner cylinder 1 of the present embodiment, by performing the metal spraying step S3 with the bent plate 10 installed, the manufacturing time can be shortened by shortening the steps. The strength of the inner cylinder 1 can be improved by the metal spraying step S3 using spray forming, and the material, shape, and plate thickness of the inner cylinder 1 can be easily selected. Furthermore, by adopting a two-layer structure for the hollow structural member 20, it is possible to simultaneously improve the workability of the hollow structural member 20, and improve the heat resistance and corrosion resistance, thereby facilitating the manufacture of the inner cylinder 1 and improving the performance. Can be achieved at the same time.

なお、例えば第三実施形態のように筒状化工程S4を備えず、プレス加工を必要としない場合には、上記第一の金属50は高延性材料に代えて高強度材料を用いてもよい。上述のトミロイ、インコネル617、Nimonic263等は高延性材料であるとともに高強度材料でもあるので、これらをそのまま用いることができる。また、さらに複数の金属材料を溶射することによって多層構造として、さらなる内筒1の材料特性の向上を図ることもできる。   For example, in the case where the cylindrical step S4 is not provided as in the third embodiment and pressing is not required, the first metal 50 may be made of a high strength material instead of the high ductility material. . The above-mentioned Tomiloy, Inconel 617, Nimonic 263, and the like are both high ductility materials and high strength materials, and thus can be used as they are. Further, by further spraying a plurality of metal materials, it is possible to further improve the material characteristics of the inner cylinder 1 as a multilayer structure.

さらに、内筒1の延在方向に材質や肉厚を変えた内筒1を製造することも可能であるので、使用環境に対応した内筒1の製造が容易に可能となる。   Furthermore, since it is also possible to manufacture the inner cylinder 1 whose material and thickness are changed in the extending direction of the inner cylinder 1, it is possible to easily manufacture the inner cylinder 1 corresponding to the use environment.

以上、本発明の実施形態についての詳細説明を行なったが、本発明の技術的思想を逸脱しない範囲内において、多少の設計変更も可能である。
上述の実施形態の説明においては、中空構造部材20を内筒1に適用したが、例えば、燃焼器100の外筒、尾筒3等の他の部位に上記中空構造部材20を適用することもできる。この際、目的とする外筒、尾筒3等の部材の形状が複雑であっても、中空構造部材20が、スプレイフォーミングによる一体成形を行って製造されるため、容易に目的とする形状にプレス加工等することが可能である。
The embodiment of the present invention has been described in detail above, but some design changes can be made without departing from the technical idea of the present invention.
In the description of the above-described embodiment, the hollow structural member 20 is applied to the inner cylinder 1. However, for example, the hollow structural member 20 may be applied to other parts such as the outer cylinder and the tail cylinder 3 of the combustor 100. it can. At this time, even if the shape of the target outer cylinder, tail cylinder 3 or the like is complicated, the hollow structural member 20 is manufactured by integral molding by spray forming, so that the target shape can be easily obtained. It can be pressed.

さらに、ガスタービン燃焼器100の燃焼室90の内筒1、外筒、尾筒3に限られず、中空構造が必要な部材に上記中空構造部材20を適用することもできる。   Furthermore, the hollow structure member 20 can be applied to a member that requires a hollow structure, not limited to the inner cylinder 1, the outer cylinder, and the tail cylinder 3 of the combustion chamber 90 of the gas turbine combustor 100.

1…内筒(筒状燃焼室)、1a…内面、1b…外面、2…バーナ、3…尾筒、4…冷却孔(中空孔)、10…屈曲板、10a…屈曲凹面、10b…屈曲凸面、20…中空構造部材、20a…端縁、21…型、21a…溝部、22…薄板(第一基板)、23…平面(第二基板)、30…セラミックコア、31…板材31、40…円筒部材(第一基板)、41…円筒外面(第二基板)、50…第一の金属、51…第二の金属、90…燃焼室、100…ガスタービン燃焼器、W…燃焼ガス、M…溶融金属、P…軸線、S1…屈曲板設置準備工程、S2…屈曲板設置工程、S3…金属溶射工程、S4…筒状化工程、S10…セラミックコア設置工程、S11…溶解工程 DESCRIPTION OF SYMBOLS 1 ... Inner cylinder (cylindrical combustion chamber), 1a ... Inner surface, 1b ... Outer surface, 2 ... Burner, 3 ... Tail cylinder, 4 ... Cooling hole (hollow hole), 10 ... Bending plate, 10a ... Bending concave surface, 10b ... Bending Convex surface, 20 ... hollow structural member, 20a ... end edge, 21 ... mold, 21a ... groove, 22 ... thin plate (first substrate), 23 ... flat surface (second substrate), 30 ... ceramic core, 31 ... plate materials 31, 40 ... cylindrical member (first substrate), 41 ... cylindrical outer surface (second substrate), 50 ... first metal, 51 ... second metal, 90 ... combustion chamber, 100 ... gas turbine combustor, W ... combustion gas, M ... Molten metal, P ... Axis, S1 ... Bending plate installation preparation step, S2 ... Bending plate installation step, S3 ... Metal spraying step, S4 ... Cylinder forming step, S10 ... Ceramic core installation step, S11 ... Melting step

Claims (5)

中空孔を有する中空構造部材の製造方法であって、
第一基板の表面上に、該表面に沿って延在するとともに該表面から突出するように屈曲する屈曲板を設置する設置工程と、
前記表面及び該表面上に配置された前記屈曲板に対して溶融金属を溶射することによって、前記第一基板に第二基板を積層する溶射工程とを備えることを特徴とする中空構造部材の製造方法。
A method for producing a hollow structural member having a hollow hole,
On the surface of the first substrate, an installation step of installing a bending plate extending along the surface and bending so as to protrude from the surface;
And a thermal spraying step of laminating a second substrate on the first substrate by spraying a molten metal on the surface and the bent plate disposed on the surface. Method.
前記屈曲板が、セラミック材料よりなり、
前記屈曲板を溶解して除去する溶解工程をさらに備えることを特徴とする請求項1に記載の中空構造部材の製造方法。
The bent plate is made of a ceramic material,
The method for producing a hollow structure member according to claim 1, further comprising a dissolving step of dissolving and removing the bent plate.
前記第一基板が、円筒形状をなし、
前記設置工程は、前記第一基板の外周面に前記屈曲板を設置する工程であり、
前記溶射工程は、前記第一基板の外周面に前記第二基板を積層する工程であることを特徴とする請求項1又は2に記載の中空構造部材の製造方法。
The first substrate has a cylindrical shape,
The installation step is a step of installing the bent plate on the outer peripheral surface of the first substrate,
The said thermal spraying process is a process of laminating | stacking said 2nd board | substrate on the outer peripheral surface of said 1st board | substrate, The manufacturing method of the hollow structure member of Claim 1 or 2 characterized by the above-mentioned.
前記第二基板が、前記第一基板側に配置される第一の金属よりなる第一金属層と、
前記第一金属層に積層され、前記第一の金属とは異なる第二の金属よりなる第二金属層とを有することを特徴とする請求項1から3のいずれか一項に記載の中空構造部材の製造方法。
The second substrate is a first metal layer made of a first metal disposed on the first substrate side;
The hollow structure according to any one of claims 1 to 3, further comprising a second metal layer that is laminated on the first metal layer and is made of a second metal different from the first metal. Manufacturing method of member.
筒状燃焼室と、該筒状燃焼室の中心に配置されて前記筒状燃焼室内へ燃料を送り込むバーナとを有する燃焼器であって、
前記筒状燃焼室が、請求項1から4のいずれか一項に記載の製造方法によって製造された中空構造部材によって形成されてなることを特徴とする燃焼器。
A combustor having a cylindrical combustion chamber and a burner that is arranged in the center of the cylindrical combustion chamber and feeds fuel into the cylindrical combustion chamber,
The combustor, wherein the cylindrical combustion chamber is formed by a hollow structural member manufactured by the manufacturing method according to any one of claims 1 to 4.
JP2011165698A 2011-07-28 2011-07-28 Method for manufacturing hollow structural member and combustor provided with hollow structural member Active JP5931368B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2011165698A JP5931368B2 (en) 2011-07-28 2011-07-28 Method for manufacturing hollow structural member and combustor provided with hollow structural member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2011165698A JP5931368B2 (en) 2011-07-28 2011-07-28 Method for manufacturing hollow structural member and combustor provided with hollow structural member

Publications (2)

Publication Number Publication Date
JP2013029077A true JP2013029077A (en) 2013-02-07
JP5931368B2 JP5931368B2 (en) 2016-06-08

Family

ID=47786320

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011165698A Active JP5931368B2 (en) 2011-07-28 2011-07-28 Method for manufacturing hollow structural member and combustor provided with hollow structural member

Country Status (1)

Country Link
JP (1) JP5931368B2 (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH10263936A (en) * 1997-03-17 1998-10-06 Westinghouse Electric Corp <We> Method for providing a passage in an object and turbomachine component
US20010001897A1 (en) * 1998-11-12 2001-05-31 Ji Cheng Zhao Method of forming hollow channels within a component
US6308765B1 (en) * 1998-11-04 2001-10-30 Grigoriy Grinberg Method of making tools having a core die and a cavity die
JP2004003017A (en) * 2002-05-07 2004-01-08 General Electric Co <Ge> Method for forming channel on surface of metallic substrate and article referring thereto
JP2005194560A (en) * 2004-01-06 2005-07-21 Mitsubishi Heavy Ind Ltd Thermal shielding film forming method, and combustor tail pipe
JP2008200836A (en) * 2007-02-22 2008-09-04 Mitsubishi Heavy Ind Ltd Metal member having hollow holes and processing method of the same
US20090220810A1 (en) * 2005-08-30 2009-09-03 Valtion Teknillinen Tutkimuskeskus Method for spray forming a metal component and a spray formed metal component

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH10263936A (en) * 1997-03-17 1998-10-06 Westinghouse Electric Corp <We> Method for providing a passage in an object and turbomachine component
US6308765B1 (en) * 1998-11-04 2001-10-30 Grigoriy Grinberg Method of making tools having a core die and a cavity die
US20010001897A1 (en) * 1998-11-12 2001-05-31 Ji Cheng Zhao Method of forming hollow channels within a component
JP2004003017A (en) * 2002-05-07 2004-01-08 General Electric Co <Ge> Method for forming channel on surface of metallic substrate and article referring thereto
JP2005194560A (en) * 2004-01-06 2005-07-21 Mitsubishi Heavy Ind Ltd Thermal shielding film forming method, and combustor tail pipe
US20090220810A1 (en) * 2005-08-30 2009-09-03 Valtion Teknillinen Tutkimuskeskus Method for spray forming a metal component and a spray formed metal component
JP2008200836A (en) * 2007-02-22 2008-09-04 Mitsubishi Heavy Ind Ltd Metal member having hollow holes and processing method of the same

Also Published As

Publication number Publication date
JP5931368B2 (en) 2016-06-08

Similar Documents

Publication Publication Date Title
EP2353763A1 (en) A method of manufacturing a hot-gas component with a cooling channel by brazing a sintered sheet on a carrier ;corresponding hot-gas component
US9422828B2 (en) Bi-cast layered wall with a porous element for component cooling
JP6431718B2 (en) Airfoil for turbine system
EP3255247B1 (en) Turbine component and methods of making and cooling a turbine component
US20120000890A1 (en) Method for repairing gas turbine blades and gas turbine blade
US20140212317A1 (en) Method of manufacturing a wall
CN104097360A (en) Configuration for joining a ceramic thermal insulating material to a metallic structure
CN109562472B (en) Method and material composite structure for joining materials
US20160059437A1 (en) Article and process for producing an article
US20110146075A1 (en) Methods for making a turbine blade
US8511991B2 (en) Composite turbine blade and method of manufacture thereof
JP2020505303A (en) Method for additionally producing fiber-reinforced ceramic matrix composite
US20110150666A1 (en) Turbine blade
CN101379345A (en) Boiler water wall panel
US9309597B2 (en) Process for applying a protective layer to a turbine component
US8240999B2 (en) Internally supported airfoil and method for internally supporting a hollow airfoil during manufacturing
JP2016188426A (en) Component parts and method for manufacturing the component parts
JP2013194694A (en) Method for repairing gas turbine moving blade and gas turbine moving blade
JP5931368B2 (en) Method for manufacturing hollow structural member and combustor provided with hollow structural member
JP5632620B2 (en) Blade manufacturing method
JP2002161755A (en) Laminating heat-resistance alloy plate and its manufacturing method
MX2014006052A (en) COOLING ELEMENT AND METHOD FOR THE MANUFACTURE OF A COOLING ELEMENT.
JP7354057B2 (en) Thermocouple mounting structure and thermocouple mounting method
US10851654B2 (en) Arrangement for a turbine
US12098691B2 (en) Combustor for rocket engine and method for manufacturing it

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20140610

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20150129

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20150203

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20150406

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A821

Effective date: 20150407

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20151013

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20151208

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A821

Effective date: 20151209

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20160405

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20160427

R151 Written notification of patent or utility model registration

Ref document number: 5931368

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R151